ONEWEB-0707, 61612
Orbit data source: Space-Track
ONEWEB-0707, 61612 is a payload satellite owned by Eut. One Web (UK) in LEO that was launched on Sun, 20 Oct 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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61612 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
UKRelated business
Manufacturer
One Web
Mission
Operational Commercial Communications
Bus & Motor
ARROW, Unknown motor
Mass
148 kg wet, ~140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 2.5 m
Radar Cross Section
2.032 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 ONEWEB-0707
1 61612U 24188U 25260.92800155 -.00000230 00000-0 -69493-3 0 9995
2 61612 87.8740 90.5293 0001882 108.0173 252.1159 13.10369376 47666Epoch: 2025-09-17T22:16Z
TLE epoch observation values (Epoch: 2025-09-17T22:16:19.333Z)
Latitude
-0.0001°
Longitude
119.35182°
Altitude
1,225.058 km
Speed
7.242 km/s
True Right ascension
06h 02m 07s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:29:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.28 km
Perigee altitude
1,217.421 km
Semi-major axis
7,596.987 km
Eccentricity
0.00019
Inclination
87.874°
RAAN
90.5293°
Arg. of periapsis
108.0173°
True anomaly
252.09538°
Mean anomaly
252.1159°
Eccentric anomaly
252.10564°
Mean motion
3.27779 °/min
Orbital period
109.83 mins
BSTAR
-0.00069493
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Other satellites on launch #188 in the year 2024 (2024-10-20 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ONEWEB-0707 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-18 11:17:41.667Z | 84.107° E | 2025-09-18 11:19:41.667Z | 67.4° ENE | 12.001° | 2025-09-18 11:21:41.667Z | 50.995° ENE |
| 12 mins | 2025-09-18 13:02:41.667Z | 170.933° S | 2025-09-18 13:07:41.667Z | 124.689° SE | 44.005° | 2025-09-18 13:14:41.667Z | 3.957° NNE |
| 7 mins | 2025-09-18 14:55:41.667Z | 256.47° W | 2025-09-18 14:58:41.667Z | 284.187° WNW | 17.296° | 2025-09-18 15:02:41.667Z | 320.597° NNW |
| 12 mins | 2025-09-19 00:32:41.667Z | 8.921° NNE | 2025-09-19 00:38:41.667Z | 99.177° ESE | 41.7° | 2025-09-19 00:44:41.667Z | 165.879° S |
| 9 mins | 2025-09-19 02:23:41.667Z | 323.884° NNW | 2025-09-19 02:27:41.667Z | 284.883° WNW | 21.254° | 2025-09-19 02:32:41.667Z | 239.168° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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